Patents by Inventor Arnaud GENILIER

Arnaud GENILIER has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Assembly comprising a locked securing stud
    Patent number: 10900382
    Abstract: An assembly includes a securing stud held by a locking key that rotates with the stud and is provided with bearing surfaces for sitting on an edge of one of the parts to be assembled.
    Type: Grant
    Filed: July 19, 2016
    Date of Patent: January 26, 2021
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Alain Dominique Gendraud, Jean-Baptiste Vincent Desforges, Arnaud Genilier, Reda Oudyi
  • ASSEMBLY COMPRISING A LOCKED SECURING STUD
    Publication number: 20180209302
    Abstract: An assembly including a securing stud held by a locking key that rotates with the stud and is provided with bearing surfaces for sitting on an edge of one of the parts to be assembled. Sufficient clamping torque can be introduced without risk of damage and at the same time avoiding excessive screwing of the stud.
    Type: Application
    Filed: July 19, 2016
    Publication date: July 26, 2018
    Applicant: SAFRAN AIRCRAFT ENGINES
    Inventors: Alain Dominique GENDRAUD, Jean-Baptiste Vincent DESFORGES, Arnaud GENILIER, Reda OUDYI
  • DEVICE FOR CONNECTING A FIXED PORTION OF A TURBINE ENGINE AND A DISTRIBUTOR FOOT OF A TURBINE ENGINE TURBINE
    Publication number: 20150315931
    Abstract: A device (1) for connecting a fixed turbine engine portion (2) and a distributor (3) foot (31) of a turbine engine turbine, comprising a ring-shaped flange (111), the flange (111) being adapted so as to be connected and secured to the fixed turbine engine portion (2) and to the foot (31) of the distributor, the device being characterized in that it further comprises a ring-shaped screen (9), the screen (9) being connected and secured to the flange (111) so as to be positioned in an upstream chamber (4) made between the fixed turbine engine portion (2) and the flange (111) so as to at least partly block heat radiation from the fixed turbine engine portion (2) and directed towards the flange (111).
    Type: Application
    Filed: October 1, 2014
    Publication date: November 5, 2015
    Applicant: SNECMA
    Inventors: Fabien GARNIER, Sebastien PRESTEL, Helene CONDAT, Patrice ROSSET, Arnaud GENILIER